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Effect of axial velocity ratio, turbulence intensity, incidence, and leading edge geometry on the midspan performance of a turbine cascade

Whitehouse, D. R., Moustapha, S. H. et Sjolander, S. A.. 1993. « Effect of axial velocity ratio, turbulence intensity, incidence, and leading edge geometry on the midspan performance of a turbine cascade ». Canadian Aeronautics and Space Journal = Journal Aéronautique et Spatial du Canada, vol. 39, nº 3. pp. 150-156.
Compte des citations dans Scopus : 10.

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Item Type: Peer reviewed article published in a journal
Professor:
Professor
Moustapha, Hany
Affiliation: Autres
Date Deposited: 02 Mar 2018 16:47
Last Modified: 02 Mar 2018 16:47
URI: http://espace2.etsmtl.ca/id/eprint/16465

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